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(2015 SV6)
Classification: Apollo [NEO]          SPK-ID: 3728645
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6420280089349143 0.00036737  
a 1.854622811213969 0.0016521 au
q .6639030204049909 8.9942e-05 au
i 5.074701217111937 0.0031145 deg
node 357.9548449636666 0.0029831 deg
peri 86.5017429039606 0.0032838 deg
M 82.41347430745174 1.0833 deg
tp 2459185.307960163737
(2020-Dec-01.80796016)
2.4939 TDB
period 922.5328137170911
2.53
1.2327
0.003375
d
yr
n .3902300217912894 0.00052143 deg/d
Q 3.045342602022947 0.0027128 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      2 days  
   first obs. used      2015-09-23  
   last obs. used      2015-09-25  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .39111  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 14:41:15  

Additional Information
 Earth MOID = .00655775 au 
 Jupiter MOID = 2.2542 au 
 T_jup = 3.717 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 27.7   n/a MPO347506  
rotation period rot_per 0.00490 h n/a LCDB (Rev. 2020-October); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Thirouin, A.; Moskovitz, N.; Binzel, R.P.; Christensen, E.; et al. (2016) Astron. J. 152, A163.]

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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